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Local Divergence-Free Immersed Finite Element-Difference Method Using Composite B-Splines

T0 review · 3 major / 6 minor · reviewed 2026-08-11 · deepseek-v4-flash

Pith's one-line read This paper claims that composite B-spline regularized delta functions in the IFED method interpolate discretely divergence-free MAC-grid velocities to continuously divergence-free fields, cutting volume-conservation error by about two…

desk verdict CBS kernels deliver real volume-conservation improvements in IFED, but the advertised divergence-free mechanism doesn't survive the FE nodal update and the abstract oversells the theory. read the letter →

arxiv 2412.15408 v1 pith:GWBIPDRJ submitted 2024-12-19 math.NA cs.NAphysics.flu-dyn

classification math.NAcs.NAphysics.flu-dyn MSC 65M6076D0574F1065D07
keywords immersedboundarymethodcompositeB-splinekernelsvolumeconservationdivergence-freeinterpolationfluid-structureinteractionregularizeddeltafunctionfiniteelement/finitedifferenceisotropickernel
verification ladder T0 review T1 audit T2 compute T3 formal

The pith

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

The reading

The paper is trying to establish that switching the regularized delta function in the immersed finite element/finite difference (IFED) method from an isotropic kernel to a composite B-spline (CBS) kernel preserves incompressibility of the immersed structure at the discrete level. In the continuous equations, an incompressible fluid automatically makes an immersed body volume-preserving, but the discrete interpolation step can introduce nonzero divergence and gradual volume loss. The paper argues that CBS kernels, built from B-splines of different orders in different coordinate directions, turn discretely divergence-free staggered-grid velocities into continuously divergence-free velocity fields, and that this removes the main source of volume error. Across pressurized-membrane, compressed-block, Cook's membrane, elastic-band, and heart-valve benchmarks, CBS kernels with no volumetric penalty or modified invariants match or beat isotropic kernels that need those stabilizations, with error reductions of roughly two orders of magnitude in the membrane test. If right, this means a kernel choice can replace algorithmic stabilization, simplifying the method and improving accuracy on coarser grids.

What carries the argument

The load-bearing object is the composite B-spline (CBS) regularized delta function: a tensor-product kernel that uses an order-$(n+1)$ B-spline in the direction of each velocity component and an order-$n$ B-spline in the transverse direction. Its defining identity is that the central difference of an order-$n$ B-spline equals the derivative of an order-$(n+1)$ B-spline, so the discrete divergence operator on the staggered marker-and-cell (MAC) grid commutes with interpolation: interpolating a discretely divergence-free velocity yields a continuously divergence-free field. The second element is the nodal quadrature scheme used for both force spreading and velocity interpolation, which makes the interpolation operator the discrete adjoint of spreading and avoids an extra projection step that could destroy the divergence-free property.

What would settle it

Run the pressurized-membrane benchmark with exactly divergence-free MAC velocities but replace the consistent nodal quadrature rule for spreading and interpolation with a different quadrature; if the enclosed-area error over one second rises to the level produced by isotropic kernels, the claim that the CBS divergence-free property survives IFED discretization is refuted. Equivalently, interpolate a discretely divergence-free MAC field with the CBS operator at arbitrary Lagrangian points and numerically compute the continuous divergence of the interpolant: nonzero values would refute the commuting property.

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Extended reading notes

Core claim

The central discovery is that the divergence-free interpolation property of composite B-spline regularized delta functions survives the IFED discretization when force spreading and velocity interpolation use consistent nodal quadrature, and that this property translates into large volume-conservation improvements. Expressed on the paper's own terms: because the central difference of an order-$n$ B-spline is the exact derivative of an order-$(n+1)$ B-spline, the componentwise asymmetric CBS interpolation maps a MAC vector field satisfying the discrete divergence equation to a continuously divergence-free interpolant. Inserting this kernel into the IFED spreading/interpolation pair makes the interpolated Lagrangian velocity divergence-free, so the solid elements are advected without spurious volume change, and the unbalanced compressive forces that generate spurious normal flows are suppressed. The paper shows this in benchmarks: pressurized membrane area error drops from roughly $10^{-5}$ to $10^{-7}$, the compressed block and Cook's membrane produce smooth displacement fields and near-unit Jacobians without volumetric energy or modified invariants, and the heart-valve model captures the same pressure and flow waveforms as stabilized isotropic kernels.

Load-bearing premise

The argument depends on the fluid solver delivering a velocity field whose discrete divergence is exactly zero on the staggered grid, and on the specific quadrature rule used to transfer quantities between grids preserving the mathematical pairing between spreading and interpolation; if either fails, the volume-conservation advantage would erode.

Editorial extensions

If this is right

  • In pressurized-membrane tests, CBS kernels reduce volume-conservation errors by about two orders of magnitude relative to isotropic IB and B-spline kernels, with little sensitivity to kernel width.
  • Without volumetric energy terms or modified invariants, CBS kernels match or beat stabilized isotropic kernels in the compressed-block and Cook's membrane benchmarks, producing near-unit Jacobians and smooth displacement fields.
  • CBS kernels converge on coarser fluid grids than isotropic kernels, and they improve as the structural mesh is refined relative to the fluid grid, whereas isotropic kernels often perform better with coarser structural meshes.
  • In the bioprosthetic heart-valve model, the wider CBS43 kernel captures high-frequency valve-flutter features comparably to or better than the isotropic B-spline kernel, while the lower-regularity CBS32 shows visible deviations during early diastole.
  • For the IFED framework, the paper recommends the CBS32 kernel with a solid-to-fluid mesh ratio of about 0.5 as a balance of accuracy and computational cost.

Reading between the lines

Editorial extensions of the paper, not claims the author makes directly.

  • The commuting property the paper relies on should transfer to any staggered-grid discretization that shares the same discrete divergence stencil, so similar volume-conservation gains may be available in other finite-difference or finite-volume fluid solvers beyond the exact setup tested here.
  • Because CBS kernels make volumetric stabilization unnecessary, unmodified constitutive invariants can be used directly, which may simplify implicit solvers and remove the artificial isotropic pressure response that modified invariants introduce into the material model.
  • The reversed mesh-ratio trend suggests a practical tuning rule with CBS kernels: refine the structural mesh rather than widening the kernel, and keep the solid-to-fluid mesh ratio at or below 0.5 near pressure-loaded interfaces.
  • A testable extension is to combine CBS kernels with higher-order structural finite elements in three dimensions; the quadrature adjointness used here was developed for nodal low-order discretizations and may need revisiting for P2 or higher bases.
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Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, and a circularity audit.

Referee Report

3 major / 6 minor

Summary. This manuscript extends the composite B-spline (CBS) regularized delta functions of Gruninger and Griffith from the classical immersed boundary method to the immersed finite element/finite difference (IFED) method. It compares CBS kernels with isotropic IB and B-spline kernels on a suite of two-dimensional benchmarks—pressurized elastic band, pressurized membrane, compressed block, Cook's membrane, slanted channel, and a modified Turek-Hron problem—as well as a three-dimensional bioprosthetic heart valve model. The central reported findings are that CBS kernels reduce volume conservation errors by roughly two orders of magnitude in pressure-loaded cases, remove the need for volumetric stabilization terms and modified invariants, converge on coarser fluid/structural meshes than isotropic kernels, and exhibit a different (in fact opposite) sensitivity to the solid-fluid mesh ratio. The authors attribute these improvements to the property, inherited from prior work, that CBS kernels interpolate discretely divergence-free MAC velocity fields to continuously divergence-free fields.

Significance. If the empirical findings hold, the paper is a useful step toward simplifying IFED simulations of incompressible hyperelastic structures: it shows that a kernel choice can reduce spurious volume change without tuning stabilization parameters. Strengths include a broad benchmark suite, validation against an analytic Poiseuille solution, comparisons with previously published displacement values, a complex 3D heart-valve test, and use of the established IBAMR infrastructure. The main weakness is that the paper presents a mechanism—exact divergence-free solid velocity—that is not actually guaranteed by the CBS construction in the IFED finite-element update; the demonstrated volume-conservation advantage is empirical and needs qualification. With that framing corrected, the benchmarks would support a weaker but still valuable claim.

major comments (3)
  1. [§3.2.2, Eqs. (15), (35)-(36)] The abstract and Section 5 state that CBS kernels 'inherently maintain the discrete divergence-free property' and produce a 'divergence-free solid velocity field.' The CBS property established in prior work is that the interpolated Eulerian field is continuously divergence-free when the MAC velocities are discretely divergence-free. In the IFED update, the structure is advected by the finite-element velocity V_h(X,t) = Σ_l φ_l(X) U_l(t), not by that interpolated Eulerian field pointwise, and for the Q1 and P1 elements used throughout the paper, div_x V_h is not identically zero even when each U_l is sampled from a continuously divergence-free field. Consequently d/dt ∫_e J_e dX = ∫_e J_e div_x V_h dX is generally nonzero, so the improved element Jacobians in Sections 4.1.2 and 4.2 are empirical reductions in interpolation/spreading error rather than a direct consequence of the CBS divergence-free theorem. Please rephrase the central claim and add a diagnostic that directly measures div_x V_h or the exact evolution of element volumes to support the proposed mechanism.
  2. [§5, Tables 1 and 4] The conclusion that CBS kernels 'eliminate the need for stabilization techniques' is too broad. In the elastic band, CBS32 fails for MFAC ≥ 1.0 (Table 1), and in the Turek-Hron benchmark, CBS32 fails for MFAC > 1.0 (Table 4); the thin-band results in Section 4.1.2 also become unstable at MFAC ≥ 1.0. The claim should be scoped to resolved configurations (e.g., MFAC < 1) and to the particular test suite, and the text should acknowledge that at coarse structural meshes CBS kernels are less robust than some isotropic kernels.
  3. [§4.1.1, Fig. 3] The 'two orders of magnitude' improvement is reported for a single grid spacing (h = 1/128) and a single final time; no grid-convergence study demonstrates that the factor persists under refinement. Since the abstract generalizes this improvement to the full test suite, either add a convergence study of the volume error for the membrane or qualify the statement so that it refers only to the shown configuration.
minor comments (6)
  1. [§1] The word 'inatroduces' in the introduction should be 'introduces'.
  2. [§3] The text 'Grifftih and Luo' in Section 3 should be 'Griffith and Luo'.
  3. [§4.2.2, Fig. 19] The caption of Figure 19 refers to the 'top-mid point of the compressed block,' but the figure reports Cook's membrane results; the caption should be corrected.
  4. [§4.3.2] The setup description contains a stray '(2)' before 'and an elastic beam'; this appears to be a formatting error.
  5. [References] Reference 48, 'PJ128117 Flory', contains an apparent artefact in the author field and should be cleaned up.
  6. [§4.3.2, Table 4] The typesetting of BS3 in Table 4 uses an inconsistent mathematical italic font ('𝐵𝑆3') compared with the rest of the table.

Circularity Check

0 steps flagged · score 0.0 of 10

No significant circularity: the CBS volume-conservation advantage rests on benchmark tests and an independently stated B-spline identity, not on a fitted input or a self-citation chain.

full rationale

The claimed derivation chain is not circular. The CBS kernel is not fitted to the volume-conservation benchmarks; it is defined by a fixed B-spline composition rule (Eqs. 35-36), and its divergence-free interpolation property is presented as a consequence of the B-spline convolution/difference identity (Eqs. 32-33), with independent precedent in Handscomb (1984) and Schroeder et al. (2022), not merely in the same-group preprint. The paper's central IFED claims are tested against external references: the pressurized membrane's zero-vorticity equilibrium state, the slanted-channel analytic Poiseuille solution, the compressed-block and Cook's-membrane solid-mechanics benchmarks, the Turek-Hron FSI benchmark, and experimental heart-valve flow and pressure traces. No parameter is fitted to the target quantity and then renamed a prediction; the only tuned parameters (penalty stiffnesses, stable time steps, numerical bulk moduli for stabilized comparisons) come from stability constraints or prior work and are not used to define the CBS kernels. The skeptic's concern that the IFED finite-element velocity field, being a C0 interpolation of nodal velocities, is not exactly divergence-free even when each nodal sample comes from a divergence-free interpolant is a correctness and robustness caveat about the strength of the advertised mechanism, not a circularity: the paper's two-order-of-magnitude volume-error reduction is an empirical benchmark result and does not reduce by construction to the kernel property. There is heavy self-citation to Gruninger and Griffith and to the same group's IFED papers, but the load-bearing mathematical facts are parameter-free and independently stated, so this does not constitute circular reasoning.

Assumptions & free parameters 3 free parameters · 5 assumptions · 0 invented entities

The central derivation introduces no fitted constants; all hand-tuned numbers are benchmark controls or stabilization terms that the paper argues CBS makes unnecessary.

free parameters (3)
  • Penalty stiffness kappa_S for boundary constraints = 2.5*2.5*dx/dt (compressed block), 0.125*dx/dt (Cook's membrane), 5e4*dx/dt^2 (Turek-Hron)
    Hand-chosen spring constants enforce displacement boundary conditions; they are numerical controls, not part of the CBS construction.
  • Numerical bulk modulus kappa_stab and Poisson ratio nu_stab = kappa_stab = 374.239 and 388.889 dyn/cm^2; nu_stab = 0.4
    Used only in the stabilized comparison runs; the central CBS claim does not depend on them.
  • Slanted channel penalty stiffness and damping = Not reported; tuned per kernel
    Selected as the largest values preserving stability for each kernel, which affects the fairness of the accuracy comparison.
assumptions (5)
  • standard math Derivative of an order-n B-spline equals the central difference of an order-(n-1) B-spline (Eq. 33).
    Standard B-spline identity used to build composite kernels.
  • domain assumption Composite B-splines interpolate discretely divergence-free MAC-grid vector fields to continuously divergence-free fields.
    Adopted from Gruninger and Griffith, Handscomb, and Schroeder et al.; not proved in this paper but used as the basis for the volume-conservation claim.
  • domain assumption The nodal quadrature scheme of Wells et al. makes the interpolation and spreading operators discrete adjoints and eliminates the need for a projection step.
    Invoked in Sections 3.1.1 and 3.2.2; if this consistency fails, the divergence-free property may not transfer to IFED.
  • domain assumption Steady-state solutions of the FSI benchmarks match the corresponding pure solid mechanics solutions.
    Used in Section 4 to validate the compression and Cook's membrane tests; assumed without proof.
  • domain assumption Equal fluid and structure densities do not affect steady-state solutions.
    Stated in Section 4 to justify using constant-coefficient solvers.

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Cite this review

Pith. "Pith review of Local Divergence-Free Immersed Finite Element-Difference Method Using Composite B-Splines." pith.science (2026). https://pith.science/paper/GWBIPDRJ

@misc{pith2026241215408,
  author       = {Pith},
  title        = {Pith review of: Local Divergence-Free Immersed Finite Element-Difference Method Using Composite B-Splines},
  year         = {2026},
  howpublished = {\url{https://pith.science/paper/GWBIPDRJ}},
  note         = {Machine review of arXiv:2412.15408}
}
read the original abstract

In the class of immersed boundary (IB) methods, the choice of the delta function plays a crucial role in transferring information between fluid and solid domains. Most prior work has used isotropic kernels that do not preserve the divergence-free condition of the velocity field, leading to loss of incompressibility of the solid when interpolating velocity to Lagrangian markers. To address this issue, in simulations involving large deformations of incompressible hyperelastic structures immersed in fluid, researchers often use stabilization approaches such as adding a volumetric energy term. Composite B-spline (CBS) kernels offer an alternative by maintaining the discrete divergence-free property. This work evaluates CBS kernels in terms of volume conservation and accuracy, comparing them with isotropic kernel functions using a construction introduced by Peskin (IB kernels) and B-spline (BS) kernels. Benchmark tests include pressure-loaded and shear-dominated flows, such as an elastic band under pressure loads, a pressurized membrane, a compressed block, Cook's membrane, and a slanted channel flow. Additionally, we validate our methodology using a complex fluid-structure interaction model of bioprosthetic heart valve dynamics. Results demonstrate that CBS kernels achieve superior volume conservation compared to isotropic kernels, eliminating the need for stabilization techniques. Further, CBS kernels converge on coarser fluid grids, while IB and BS kernels need finer grids for comparable accuracy. Unlike IB and BS kernels, which perform better with larger mesh ratios, CBS kernels improve with smaller mesh ratios. Wider kernels provide more accurate results across all methods, but CBS kernels are less sensitive to grid spacing variations than isotropic kernels.

Figures

Figures reproduced from arXiv: 2412.15408 by the authors.

Figure 1
Figure 1. Pressurized membrane setup. The circular membrane (radius 0.25) at equilibrium experiences a pressure difference across its interface, with interior pressure 𝑝𝑖 and exterior pressure 𝑝𝑜 [PITH_FULL_IMAGE:figures/full_fig_p013_1.png] view at source ↗
Figure 2
Figure 2. Vorticity comparison between IB4 (left) and CBS43 (right) of for the pressurized thin elastic membrane. The vorticity should ideally be zero everywhere. The CBS kernel exhibits a noticeably smaller error induced by non-zero velocity due to errors in the discrete force spreading operator. 13 [PITH_FULL_IMAGE:figures/full_fig_p013_2.png] view at source ↗
Figure 3
Figure 3. Volume conservation comparison of pressurized thin elastic membrane for different kernels. To examine the sensitivity of grid spacing ratios between the solid and fluid meshes (MFAC), we fix the fluid grid with a high resolution (𝑁 = 128) and vary MFAC as 0.5, 0.75, 1.0, 1.25, and 1.5 [PITH_FULL_IMAGE:figures/full_fig_p014_3.png] view at source ↗
Figures from the paper (25 more)
Figure 4
Figure 4. Figure 4: The effects of MFAC on the volume conservation error of pressurized thin elastic membrane for different kernels. 4.1.2 Two-dimensional Pressure-loaded Elastic Band This benchmark examines the deformation of a thin immersed elastic band under pressure loading, which pre…
Figure 5
Figure 5. Figure 5: Schematic of a two-dimensional pressure-loaded elastic band. The elastic band is fixed at the top and bottom and experiences pressure differences across the band [PITH_FULL_IMAGE:figures/full_fig_p015_5.png]
Figure 6
Figure 6. Figure 6: Comparison of the influence of MFAC on the volume conservation of the pressure-loaded elastic band to isotropic kernels. (a) IB5 and (b) BS6. Generally, smaller MFAC yields better results regarding the volume conservation for all kernels. There are indistinct differenc…
Figure 7
Figure 7. Figure 7: Comparison of the influence of MFAC on the volume conservation of the pressure-loaded elastic band using CBS32 with MFAC = 0.2, 0.5, 0.75, and 1.0 (left to right). Compared with isotropic kernels ( [PITH_FULL_IMAGE:figures/full_fig_p017_7.png]
Figure 8
Figure 8. Figure 8: The deformation of the elastic band for CBS32 at 𝑡 = 0.2 s for different MFAC values. The color map represents the elemental Jacobian values. At MFAC = 0.5, the elastic band deforms smoothly and the elemental Jacobians remain close to unity. As MFAC increases to 1.0 an…
Figure 9
Figure 9. Figure 9: Comparison of stabilization treatments for CBS32 with MFAC = 0.5 (𝑡 = 10 s), visualized through element Jacobian distributions: (a) without a volumetric penalty term and using unmodified invariants, (b) including only a volumetric penalty term, (c) using modified invar…
Figure 10
Figure 10. Figure 10: Schematic of the compressed block benchmark The discretization uses a uniform Cartesian grid with 𝑁 = ⌈𝑀 · MFAC⌉ cells per direction, where 𝑀 is the number of Q 1 elements along the longest edge of the Lagrangian mesh. We examine cases with 𝑀 = 4, 8, 16, 32, 48, and 6…
Figure 11
Figure 11. Figure 11: The comparison of the Jocobians between the unmodified invariants with omitting the volumetric energy (left column) and with both treatments (right column) for different kernels (𝑡 = 100 s). The special treatments improve IB3 and BS3 a lot for volume conservation but …
Figure 12
Figure 12. Figure 12: The comparison of the displacement between the unmodified invariants with omitting the volumetric energy (left column) and with both treatments (right column) for different kernels. The special treatments improve IB3 and BS3 a lot for volume conservation but have litt…
Figure 13
Figure 13. Figure 13: The comparison of the vertical displacements at the center of the top surface with and without the volumetric stabilization treatments for different kernels with 𝑀 = 32 and MFAC = 0.5 for the compressed block benchmark. The displacement of the top-mid point is similar…
Figure 14
Figure 14. Figure 14: Grid convergence with different MFAC in terms of the displacement of the probed location. These are the results without modified invariants or volumetric energies. (1) Grid convergence is better for smaller MFACs for all kernels, but CBS kernels converge at a coarse m…
Figure 15
Figure 15. Figure 15: Error norms of Jacobian against MFAC with 𝑁 = 90. All kernel types show convergence under solid mesh refinement, with wider kernels yielding smaller errors. CBS kernels generally demonstrate superior volume conservation across different MFAC values, except for IB6 whi…
Figure 16
Figure 16. Figure 16: Setup of the Cook’s membrane benchmark problem. The 𝑦-displacement at the upper-right corner (indicated by the circle) is monitored for subsequent analysis. The initial configuration of the structure, denoted by Ω 𝑠 0 , is immersed within the fluid domain Ω 𝑓 0 . The …
Figure 17
Figure 17. Figure 17: The comparison of the Jocobians between the unmodified invariants with no volumetric energy (left column) and with both treatments (right column) for different kernels (MFAC = 0.5, 𝑡 = 50 s). The special treatments improve IB3 and BS3 a lot for volume conservation but…
Figure 18
Figure 18. Figure 18: The displacement comparison between the unmodified invariants with no volumetric energy (left column) and with both treatments (right column) for different kernels (MFAC = 0.5, 𝑡 = 50 s). The special treatments improve IB3 and BS3 a lot for volume conservation but hav…
Figure 19
Figure 19. Figure 19: Comparison of the displacement at the top-mid point of the compressed block with and without volumetric energy and stabilization treatments for different kernels. A clear difference is observed between cases with and without these treatments for IB and BS kernels, whi…
Figure 20
Figure 20. Figure 20: All kernels achieve grid convergence as the grid is refined across different MFAC values. CBS kernels demonstrate consistent performance and are less sensitive to MFAC, achieving convergence on coarser grids with better results at smaller MFAC values. In contrast, IB …
Figure 21
Figure 21. Figure 21: Error norms of the Jacobian as a function of MFAC with 𝑁 = 90. IB and BS kernels show improved results with larger MFAC values, while CBS kernels display the opposite trend, with smaller MFAC values yielding lower errors. Additionally, different CBS kernels exhibit le…
Figure 22
Figure 22. Figure 22: Computational setup of the slanted channel flow problem (inclination angle 𝜋/6). The color map shows the velocity field computed using CBS32 kernel. The white vertical line at 𝑥 = 0.5 indicates the location of velocity profile measurements, and the dots represent Lagr…
Figure 23
Figure 23. Figure 23: Comparison of velocity profiles at 𝑥 = 0.5 for different kernel types. Kernels with narrower support regions show better accuracy in capturing peak velocities, with BS and CBS kernels of equal support performing similarly and outperforming their IB counterparts. The w…
Figure 24
Figure 24. Figure 24: Schematic of the Turek-Hron benchmark The boundary conditions are specified as follows: at the inlet (𝑥 = 0), 𝑢(0, 𝑦) = 1.5𝑈 𝑦(𝐻 − 𝑦)/(𝐻/2) 2 , where 𝑈 = 2 is the average velocity; at the outlet (𝑥 = 𝐿), zero normal traction and zero tangential velocity are imposed; a…
Figure 25
Figure 25. Figure 25: presents a representative color map of the vorticity field, highlighting the deformed beam simulated with the CBS32 kernel and MFAC = 0.5 [PITH_FULL_IMAGE:figures/full_fig_p037_25.png]
Figure 26
Figure 26. Figure 26: Vertical displacement of point 𝐴 (as shown in [PITH_FULL_IMAGE:figures/full_fig_p038_26.png]
Figure 27
Figure 27. Figure 27: Representative cross section views of simulated axial velocity for the bioprosthetic heart valve model The boundary conditions include three-element Windkessel models for upstream driving and downstream loading conditions of the aortic test section, as detailed previo…
Figure 28
Figure 28. Figure 28: compares the aortic and left ventricular pressures, along with flow rates obtained using different kernels. Before valve flutter (𝑡 < 0.35 s), the results show a minimal discrepancy between the kernels, and the predicted flow rates demonstrate good agreement with expe…

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Cited by 1 Pith paper

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